The influence of surface ply fibre angle on the compressive strength of composite laminates containing delamination (2016)
Attributed to:
Aerostructural Efficiency of Damage Tolerant Composites via Optimised Fibre Placement
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Digital Object Identifier: http://dx.doi.org/10.1017/s000192400000765x
Publication URI: http://dx.doi.org/10.1017/s000192400000765x
Type: Journal Article/Review
Parent Publication: The Aeronautical Journal
Issue: 1186
ISSN: 00019240